STARLINK-30360 (57776)

COSPAR: 2023-134F | Alt Name: Starlink 30360

Image
STARLINK-30360 Satellite Image
Additional Sources
Launch Details

Launch Date

September 4, 2023

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

57776

International Designator

2023-134F

Epoch

Sun, 19 Jul 2026 07:31:23 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

171.43°

Eccentricity

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Argument of Perigee

274.82°

Period

94.27 min

Mean Motion

15.28 rev/day

Latitude

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Longitude

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Altitude

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Velocity

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Polar Plot
3D Visualization
Basic Satellite Info

Name

STARLINK-30360

Alternative Name

Starlink 30360

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 57776U 23134F   26200.31347214  .00000749  00000+0  36731-4 0  9993
2 57776  43.0032 171.4334 0001506 274.8210  85.2470 15.27577150159635

Source: Celestrak

Summary
The STARLINK-30360 satellite, also known as Starlink 30360, is a communication satellite belonging to the Starlink v2 Mini configuration and part of the Starlink Group 6-12-06 payload. Launched on September 4, 2023, from LC39A at AFETR using a Falcon 9 launch vehicle, it has a length of 0.3 meters, a diameter of 4.1 meters, and a span of 29 meters. Its dry mass is 700 kg with a launch mass of 730 kg. The satellite is powered by solar arrays and batteries and is equipped with Ku/Ka/E-band payload and an optical inter-satellite link for communication purposes. It uses Argon ion thrusters as its motor system. Manufactured by SPXS, the satellite's owner is also SpaceX (SPXS).

Starlink is a satellite constellation developed by SpaceX with the aim of providing global broadband internet coverage. Thousands of small satellites are deployed in low Earth orbit (LEO), enabling high-speed internet access even in remote areas. However, the rapid increase in satellites raises concerns about space debris and the potential for collisions, which can lead to further debris creation and endanger other spacecraft. Additionally, the sheer number of Starlink satellites can affect astronomical observations by increasing light pollution. Proper deorbiting plans and international coordination are essential to mitigate these challenges and ensure long-term sustainability in space.
Physical Characteristics

Length

0.3

Diameter

4.1

Span

29

Dry Mass

700

Launch Mass

730

Shape

Box + pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Starlink Group 6-12-06

Purpose

Communication

Mission

Communication

Manufacturer

SPXS

Life Expectancy

Unknown

Bus

Starlink V2M

Configuration

Starlink v2 Mini

Motor

Argon ion thrusters

Equipment

Ku/Ka/E-band payload, optical inter-satellite link

Power System

Solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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